Described are aircraft passenger seat assemblies with a passenger seat, a component with an outer surface attached the passenger seat. An inductive wireless power unit with a coil assembly is included with the aircraft passenger seat assembly, and the coil assembly is positioned within the component. A portion of the outer surface of the component covers the coil assembly. Wires connecting the coil assembly to a power supply are hidden from view within the aircraft passenger seat assembly.

An object position determining system, applied to a vehicle, comprising: at least one light source, configured to emit light; at least one optical sensor, configured to sense optical data generated based on reflected light of the light; and a processing circuit, configured to compute distance information between the optical sensor and at least one object which generates the reflected light, and real time vehicle orientation data; wherein the processing circuit determines at least one position of the object according to the distance information and the real time vehicle orientation data.

A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

A tray table apparatus includes a table carrier structure releasably mountable to a console element, wherein the table carrier structure is configured as a housing. The tray table apparatus further includes an adjustment mechanism housed within the table carrier structure, wherein the adjustment mechanism has a table support element movable relative to the table carrier structure. The tray table apparatus also includes a table element coupled to the table support element and together movable between at least a retracted stowed position in which the table element is housed within the table carrier structure and a deployed use position in which the table element protrudes from the table carrier structure.

An aircraft seat device has a multi-part backrest frame unit comprising at least one first side frame element, at least one second side frame element, which is arranged on a side of the backrest frame unit that is opposite from the first side frame element, and at least one transverse frame element which is realized separately from the side frame elements and connects the side frame elements, wherein the transverse frame element is realized at least substantially plate-shaped.

A seating assembly may employ one or more of: a seat stagger, a seat overlap, and a seat angling to offer significant width and comfort gains and reduce the negative impact of width and leg room gains on seating density. With one seat of a pair staggered forward with respect to the other seat each may then be moved laterally and overlap (as seen from the front). The seating positions may be further improved by angling each seat away from their center arm rest area, reducing the encroaching effect of the overlap by pointing the passenger away from the overlap, reducing the visual impact of the staggered seating by pointing the passenger away from the nearest seat ahead, and improving leg room by directing the passenger's legs forward at an angle.

A telescopic rail system includes rails slidably interconnected with each other such that the rails slide relative to each other along a longitudinal axis. The rails are configured to be operatively connected to a carriage such that the rails guide movement of the carriage between an extended position and a retracted position. The rails include first and second magnetic detents configured to releasably hold the carriage in a partially-extended position and the extended position, respectively.

A detent mechanism is provided for a tray table of an aircraft. The detent mechanism includes an actuator configured to move along with a table leaf of the tray table as the table leaf rotates between a stowed position and a deployed position of the table leaf. The detent mechanism includes a follower biased toward an open position of the follower. The follower is configured to be moved against the bias from the open position into a closed position of the follower by engagement of the actuator with the follower as the table leaf rotates from the stowed position into the deployed position. The follower includes a magnetic component configured to releasably hold the follower in the closed position.

Described is a passenger seat having a seat member moveable between a stowed position and a deployed position and at least one actuator coupled to at least one portion of the seat member, wherein the at least one actuator is activable without direct contact with a passenger's hand to change a lock state of the seat member, and wherein an unlocked state of the seat member permits movement of the seat member between the stowed position and the deployed position.

Described are tray tables having a shroud and a core assembly. The shroud may form an outer surface of the tray table. The core assembly may be within the shroud and may include a top sheet, a bottom sheet, and a honeycomb core. The honeycomb core may be between the top sheet and the bottom sheet. The honeycomb core may define a plurality of cells.